BRPI0612522A2 - processo de detecção de vazamento de combustìvel em um motor de aeronave e sistema de aplicação desse processo - Google Patents

processo de detecção de vazamento de combustìvel em um motor de aeronave e sistema de aplicação desse processo Download PDF

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Publication number
BRPI0612522A2
BRPI0612522A2 BRPI0612522-0A BRPI0612522A BRPI0612522A2 BR PI0612522 A2 BRPI0612522 A2 BR PI0612522A2 BR PI0612522 A BRPI0612522 A BR PI0612522A BR PI0612522 A2 BRPI0612522 A2 BR PI0612522A2
Authority
BR
Brazil
Prior art keywords
engine
fuel
consumption
aircraft
process according
Prior art date
Application number
BRPI0612522-0A
Other languages
English (en)
Portuguese (pt)
Inventor
Jean-Luc Rivot
Original Assignee
Airbus France
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus France filed Critical Airbus France
Publication of BRPI0612522A2 publication Critical patent/BRPI0612522A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/005—Accessories not provided for in the groups B64D37/02 - B64D37/28
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/46—Emergency fuel control
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M3/00—Investigating fluid-tightness of structures
    • G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
    • G01M3/025—Details with respect to the testing of engines or engine parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/80—Diagnostics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/09—Purpose of the control system to cope with emergencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Examining Or Testing Airtightness (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
BRPI0612522-0A 2005-06-21 2006-06-20 processo de detecção de vazamento de combustìvel em um motor de aeronave e sistema de aplicação desse processo BRPI0612522A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0551696 2005-06-21
FR0551696A FR2887226B1 (fr) 2005-06-21 2005-06-21 Procede de detection de fuite de carburant dans un moteur d'aeronef et systeme de mise en oeuvre de ce procede
PCT/FR2006/001467 WO2006136736A2 (fr) 2005-06-21 2006-06-20 Procede de detection de fuite de carburant dans un moteur d'aeronef et systeme de mise en œuvre de ce procede

Publications (1)

Publication Number Publication Date
BRPI0612522A2 true BRPI0612522A2 (pt) 2010-11-23

Family

ID=35976687

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0612522-0A BRPI0612522A2 (pt) 2005-06-21 2006-06-20 processo de detecção de vazamento de combustìvel em um motor de aeronave e sistema de aplicação desse processo

Country Status (11)

Country Link
US (1) US8387440B2 (fr)
EP (1) EP1893487B1 (fr)
JP (1) JP4682243B2 (fr)
CN (1) CN100503369C (fr)
AT (1) ATE437802T1 (fr)
BR (1) BRPI0612522A2 (fr)
CA (1) CA2611993C (fr)
DE (1) DE602006008140D1 (fr)
FR (1) FR2887226B1 (fr)
RU (1) RU2397920C2 (fr)
WO (1) WO2006136736A2 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7739004B2 (en) 2006-11-29 2010-06-15 The Boeing Company Automatic engine fuel flow monitoring and alerting fuel leak detection method
DE102008058451B4 (de) * 2008-11-21 2010-11-18 Airbus Deutschland Gmbh Verfahren und System zur Notbelüftung einer Flugzeugkabine im Fall eines Lecks im Bereich eines Luftmischers
US10031042B2 (en) * 2009-08-18 2018-07-24 Innovative Pressure Testing, Llc System and method for detecting leaks
ES2723710T3 (es) 2013-10-17 2019-08-30 Innovative Pressure Testing Llc Sistema y método para una prueba de presión de referencia
CA2926187C (fr) 2013-10-17 2020-01-07 Innovative Pressure Testing, Llc Systeme et procede pour un test de performances de pression
CN103822763A (zh) * 2014-03-06 2014-05-28 中国商用飞机有限责任公司 用于飞机燃油链路中的燃油泄漏的检测方法
DE102014119210A1 (de) * 2014-12-19 2016-06-23 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Ermittlung eines Treibstofflecks eines Treibstoffsystems eines wenigstens zwei Triebwerke aufweisenden Flugzeugs
US10260425B2 (en) * 2016-05-05 2019-04-16 United Technologies Corporation Leak detection, isolation and accommodation assembly for gas turbine engines
IT201700073686A1 (it) * 2017-06-30 2018-12-30 Nuovo Pignone Tecnologie Srl Metodo e sistema per l'avvio sicuro di turbine a gas
CA3079764A1 (fr) 2017-10-23 2019-05-02 Bombardier Inc. Systeme et procede de detection de fuite de carburant dans un aeronef
FR3128993B1 (fr) 2021-11-08 2024-02-16 Safran Aerosystems Système de détection de fuites, notamment pour un système carburant d’un aéronef, et procédé de détection d’une fuite de carburant

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5297423A (en) * 1992-07-27 1994-03-29 Integrated Product Systems, Inc. Storage tank and line leakage detection and inventory reconciliation method
JPH07286930A (ja) * 1994-04-18 1995-10-31 Japan Airlines Co Ltd 航空機における燃料漏れ位置の検出方法及びこれに用いる装置
US6837744B2 (en) * 2002-03-13 2005-01-04 Hydro-Aire, Inc. Electrical connector for aircraft fuel pumps
RU2240263C1 (ru) * 2003-06-10 2004-11-20 Открытое акционерное общество "ОКБ Сухого" Способ оповещения экипажа об утечке топлива на ла в полете
US8074627B2 (en) * 2010-07-14 2011-12-13 Ford Global Technologies, Llc Automotive fuel system leak testing

Also Published As

Publication number Publication date
CN100503369C (zh) 2009-06-24
DE602006008140D1 (de) 2009-09-10
RU2397920C2 (ru) 2010-08-27
US8387440B2 (en) 2013-03-05
JP4682243B2 (ja) 2011-05-11
JP2008544154A (ja) 2008-12-04
RU2008102131A (ru) 2009-07-27
FR2887226B1 (fr) 2008-08-08
FR2887226A1 (fr) 2006-12-22
WO2006136736A3 (fr) 2007-03-15
EP1893487B1 (fr) 2009-07-29
EP1893487A2 (fr) 2008-03-05
US20100288883A1 (en) 2010-11-18
WO2006136736A2 (fr) 2006-12-28
ATE437802T1 (de) 2009-08-15
CA2611993C (fr) 2013-01-08
CN101203426A (zh) 2008-06-18
CA2611993A1 (fr) 2006-12-28

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

Free format text: TRANSFERIDO POR INCORPORACAO DE: AIRBUS FRANCE

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]